US4543885A - Increment charge for a finned projectile - Google Patents
Increment charge for a finned projectile Download PDFInfo
- Publication number
- US4543885A US4543885A US06/474,030 US47403083A US4543885A US 4543885 A US4543885 A US 4543885A US 47403083 A US47403083 A US 47403083A US 4543885 A US4543885 A US 4543885A
- Authority
- US
- United States
- Prior art keywords
- discs
- powder
- cartridge tube
- cartridge
- ignition
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/08—Ordnance projectiles or missiles, e.g. shells
- F42B30/10—Mortar projectiles
- F42B30/12—Mortar projectiles with provision for additional propulsive charges, or for varying the length
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
Definitions
- the present invention relates to an increment charge for a finned projectile designed to surround a cartridge tube in the projectile and be ignited by the ignition gases from a propellant and ignition cartridge included in the cartridge tube.
- a customary embodiment of increment charges for finned projectiles consists of a crushed powder which is punched into shapes similar to a horeshoe. These charges contain a number of relatively thin such discs, normally grouped together in a textile covering.
- the internal horseshoe-shape is substantially circular (an open circle) and somewhat larger than the cartridge tube.
- a selected number of such increment charges, together with a propellant and ignition cartridge arranged in the cartridge tube, comprise the total charge for ejecting the projectile from a barrel.
- the cartridge tube is provided with holes through which the combustion gases from the said cartridge flow outwards to the increment charges in order to ignite these.
- increment charge powder discs should be effectively ignited over as large a portion of the surface of the individual powder discs as possible.
- the ignition unit the propellant and ignition cartridge
- gas which flows outwards through the system of holes in the cartridge tube will primarily encounter the relatively compacted inner edge surface of the powder pack and will then subsequently spread outwards to the "major surfaces" of the discs.
- This ignition of the "major surfaces” presupposes that the ignition gases can easily penetrate in between the individual discs.
- the object of the present invention is to provide an increment charge which, thanks to extremely simple and cheap shaping of the increment charge, provides particularly good access facilities for the ignition gases flowing outwards from the propellant and ignition cartridge.
- FIG. 1 provides a side view, partly in longitudinal section, of the rear portion of a conventional finned projectile provided with a number of increment charges in accordance with the invention.
- FIG. 2 provides a plan view of the powder disc which forms part of an increment charge in accordance with an invention.
- FIGS. 3-4 show schematically in plan view and in perspective respectively an arrangement of several powder discs in accordance with FIG. 2.
- FIG. 1 illustrates the rear portion of a conventional finned projectile 1 with a cartridge tube 2.
- the cartridge tube 2 is provided in a conventional manner with a guidance mechanism 3, which is shown only partially, and includes a conventional propellant and ignition cartridge 4 which is shown only schematically.
- the wall of the cartridge tube 2 has a number of apertures 5 so as to permit the outward flow of the ignition gases from the cartridge 4 to a number (eight in the example shown) of increment charges 6 in accordance with the invention.
- Each increment charge 6 consists of a number (in the example shown here eight) of horseshoe-shaped powder discs 7, having their "major surfaces" placed against each other, provided with respective central holes, and preferably enclosed in a conventional textile covering and pushed around the cartridge tube 2.
- FIGS. 2-4 A preferred embodiment of the individual powder discs 7 is illustrated in FIGS. 2-4. So as to provide a more detailed explanation of the mutual arrangement of the powder discs 7 in the increment charges 6, FIG. 2 illustrates a single such disc 7 pushed around the cartridge tube 2, whilst FIG. 3 illustrates the mutual arrangement of two such discs and FIG. 4 illustrates a perspective view of a pack of five such discs 7.
- each of the powder discs 7 has the shape of a centrally-located square 8 with radiussed corners 9, where the square 8 has been rotated through an angle ⁇ of appropriately about 30° relative to the "horseshoe aperture" 10 of the disc.
- a pack is obtained as shown in FIGS. 3 and 4 where a number of recesses 11 are obtained in the pack of discs because the corner edge portions 9 in each disc are located at a greater distance from the cartridge tube 2 than the nearest edge portions of adjacent discs, with alternate discs inverted or rotated as shown in FIGS. 3 and 4 so that the form or shape of the hole edge is inverted in mirror fashion for each second or alternate discs.
- the same access surface for the ignition gases can naturally also be provided by ramming the powder discs 7 in two different inner edge shapes which are placed against each other (not shown).
- the inner shape of all discs 7 is circular, but with a smaller diameter for each second or for each second and third disc.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Air Bags (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
Abstract
Description
Claims (1)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8202085 | 1982-04-01 | ||
SE8202085A SE427695B (en) | 1982-04-01 | 1982-04-01 | PART CHARGING FOR A WING GRANDE |
Publications (1)
Publication Number | Publication Date |
---|---|
US4543885A true US4543885A (en) | 1985-10-01 |
Family
ID=20346437
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US06/474,030 Expired - Fee Related US4543885A (en) | 1982-04-01 | 1983-03-10 | Increment charge for a finned projectile |
Country Status (5)
Country | Link |
---|---|
US (1) | US4543885A (en) |
EP (1) | EP0090954B1 (en) |
DE (1) | DE3362138D1 (en) |
NO (1) | NO150057C (en) |
SE (1) | SE427695B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4887534A (en) * | 1988-06-10 | 1989-12-19 | Honeywell Inc. | Ignition system for high intrusion projectile |
US5367872A (en) * | 1993-04-27 | 1994-11-29 | Thiokol Corporation | Method and apparatus for enhancing combustion efficiency of solid fuel hybrid rocket motors |
US20050268806A1 (en) * | 2004-02-09 | 2005-12-08 | Patria Vammas Oy | Increment charge for fin-stabilized mortar projectile |
US20160010966A1 (en) * | 2013-02-22 | 2016-01-14 | Bae Systems Bofors Ab | Shell with ejectable shell base |
RU2601662C1 (en) * | 2015-05-21 | 2016-11-10 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | COMMON FULL ADJUSTABLE CHARGE FOR 82-mm MORTAR ROUND |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19750071A1 (en) * | 1997-11-12 | 1999-05-20 | Dynamit Nobel Ag | Propellant charge container |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1883758A (en) * | 1929-11-09 | 1932-10-18 | Brandt Edgar William | Bladed projectile |
US2069794A (en) * | 1933-06-05 | 1937-02-09 | David L Woodberry | Shell for firearms |
GB496792A (en) * | 1937-03-31 | 1938-12-06 | Jean Fabry | Improvements in projectiles provided with tail-fins |
US2210959A (en) * | 1938-10-24 | 1940-08-13 | Christian G Storm | Propellent charge holder |
US2620732A (en) * | 1944-11-29 | 1952-12-09 | Clarence N Hickman | Mortar charge |
US2721518A (en) * | 1945-01-26 | 1955-10-25 | Clarence N Hickman | Projectile |
US2918005A (en) * | 1956-10-31 | 1959-12-22 | Schecter George | Sheet propellant |
US3017836A (en) * | 1958-08-28 | 1962-01-23 | Phillips Petroleum Co | Rocket motor |
US3638571A (en) * | 1967-09-06 | 1972-02-01 | Dynamit Nobel Ag | Recoilless practice cartridge |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB122509A (en) * | 1918-02-08 | 1919-01-30 | Frederick Wilfrid Scott Stokes | Improvements in or relating to Projectiles. |
FR692609A (en) * | 1929-04-05 | 1930-11-07 | Anciens Ets Skoda | Process for firing charges and their arrangement in cartridge cases |
DE1141923B (en) * | 1960-01-28 | 1962-12-27 | Hotchkiss Brandt Fa | Additional charge for projectiles with a tubular tail part |
DE2051574C3 (en) * | 1970-10-21 | 1974-05-02 | Oy Tampella Ab, Tampere (Finnland) | Wing-stabilized projectile for launchers, mortars and the like |
-
1982
- 1982-04-01 SE SE8202085A patent/SE427695B/en not_active IP Right Cessation
-
1983
- 1983-03-07 EP EP83102222A patent/EP0090954B1/en not_active Expired
- 1983-03-07 DE DE8383102222T patent/DE3362138D1/en not_active Expired
- 1983-03-10 US US06/474,030 patent/US4543885A/en not_active Expired - Fee Related
- 1983-03-23 NO NO831021A patent/NO150057C/en unknown
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1883758A (en) * | 1929-11-09 | 1932-10-18 | Brandt Edgar William | Bladed projectile |
US2069794A (en) * | 1933-06-05 | 1937-02-09 | David L Woodberry | Shell for firearms |
GB496792A (en) * | 1937-03-31 | 1938-12-06 | Jean Fabry | Improvements in projectiles provided with tail-fins |
US2210959A (en) * | 1938-10-24 | 1940-08-13 | Christian G Storm | Propellent charge holder |
US2620732A (en) * | 1944-11-29 | 1952-12-09 | Clarence N Hickman | Mortar charge |
US2721518A (en) * | 1945-01-26 | 1955-10-25 | Clarence N Hickman | Projectile |
US2918005A (en) * | 1956-10-31 | 1959-12-22 | Schecter George | Sheet propellant |
US3017836A (en) * | 1958-08-28 | 1962-01-23 | Phillips Petroleum Co | Rocket motor |
US3638571A (en) * | 1967-09-06 | 1972-02-01 | Dynamit Nobel Ag | Recoilless practice cartridge |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4887534A (en) * | 1988-06-10 | 1989-12-19 | Honeywell Inc. | Ignition system for high intrusion projectile |
US5367872A (en) * | 1993-04-27 | 1994-11-29 | Thiokol Corporation | Method and apparatus for enhancing combustion efficiency of solid fuel hybrid rocket motors |
US20050268806A1 (en) * | 2004-02-09 | 2005-12-08 | Patria Vammas Oy | Increment charge for fin-stabilized mortar projectile |
US7690305B2 (en) * | 2004-02-09 | 2010-04-06 | Patria Vammas Oy | Increment charge for fin-stabilized mortar projectile |
AU2005210782B2 (en) * | 2004-02-09 | 2010-11-11 | Patria Weapon Systems Oy | Increment charge for fin-stabilized mortar projectile |
AU2005210782B8 (en) * | 2004-02-09 | 2011-03-10 | Patria Weapon Systems Oy | Increment charge for fin-stabilized mortar projectile |
US20160010966A1 (en) * | 2013-02-22 | 2016-01-14 | Bae Systems Bofors Ab | Shell with ejectable shell base |
US9448048B2 (en) * | 2013-02-22 | 2016-09-20 | Bae Systems Bofors Ab | Shell with ejectable shell base |
RU2601662C1 (en) * | 2015-05-21 | 2016-11-10 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | COMMON FULL ADJUSTABLE CHARGE FOR 82-mm MORTAR ROUND |
Also Published As
Publication number | Publication date |
---|---|
EP0090954A1 (en) | 1983-10-12 |
SE427695B (en) | 1983-04-25 |
NO150057C (en) | 1984-08-08 |
DE3362138D1 (en) | 1986-03-27 |
NO831021L (en) | 1983-10-03 |
NO150057B (en) | 1984-04-30 |
EP0090954B1 (en) | 1986-02-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: FORENADE FABRIKSVERKEN; S-631 ESKILSTUNA, SWEDEN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNORS:AKHAGEN, RUNE;JANSSON, ARTHUR;REEL/FRAME:004106/0999 Effective date: 19830304 |
|
FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
FEPP | Fee payment procedure |
Free format text: PAYER NUMBER DE-ASSIGNED (ORIGINAL EVENT CODE: RMPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
LAPS | Lapse for failure to pay maintenance fees | ||
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 19931003 |
|
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |